CN1228484C - Carbon fluoride fibre, active matter and solid lubricating material for battery using the same - Google Patents
Carbon fluoride fibre, active matter and solid lubricating material for battery using the same Download PDFInfo
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- CN1228484C CN1228484C CNB021074992A CN02107499A CN1228484C CN 1228484 C CN1228484 C CN 1228484C CN B021074992 A CNB021074992 A CN B021074992A CN 02107499 A CN02107499 A CN 02107499A CN 1228484 C CN1228484 C CN 1228484C
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- 239000000835 fiber Substances 0.000 title claims description 97
- 239000007787 solid Substances 0.000 title claims description 6
- 239000000463 material Substances 0.000 title description 3
- 230000001050 lubricating effect Effects 0.000 title 1
- TXEYQDLBPFQVAA-UHFFFAOYSA-N tetrafluoromethane Chemical compound FC(F)(F)F TXEYQDLBPFQVAA-UHFFFAOYSA-N 0.000 title 1
- 229910052799 carbon Inorganic materials 0.000 claims abstract description 146
- OKTJSMMVPCPJKN-UHFFFAOYSA-N Carbon Chemical compound [C] OKTJSMMVPCPJKN-UHFFFAOYSA-N 0.000 claims abstract description 139
- QLOAVXSYZAJECW-UHFFFAOYSA-N methane;molecular fluorine Chemical compound C.FF QLOAVXSYZAJECW-UHFFFAOYSA-N 0.000 claims description 28
- 238000009825 accumulation Methods 0.000 claims description 22
- 238000001947 vapour-phase growth Methods 0.000 claims description 9
- 239000011149 active material Substances 0.000 claims description 7
- 239000000314 lubricant Substances 0.000 claims description 5
- VNWKTOKETHGBQD-UHFFFAOYSA-N methane Chemical class C VNWKTOKETHGBQD-UHFFFAOYSA-N 0.000 abstract description 7
- 239000010410 layer Substances 0.000 description 53
- 238000010438 heat treatment Methods 0.000 description 13
- UHOVQNZJYSORNB-UHFFFAOYSA-N Benzene Chemical compound C1=CC=CC=C1 UHOVQNZJYSORNB-UHFFFAOYSA-N 0.000 description 9
- 238000005087 graphitization Methods 0.000 description 9
- PXHVJJICTQNCMI-UHFFFAOYSA-N Nickel Chemical compound [Ni] PXHVJJICTQNCMI-UHFFFAOYSA-N 0.000 description 8
- 230000000694 effects Effects 0.000 description 8
- 238000001069 Raman spectroscopy Methods 0.000 description 7
- 238000010586 diagram Methods 0.000 description 7
- 238000001228 spectrum Methods 0.000 description 7
- 239000000654 additive Substances 0.000 description 6
- 150000001721 carbon Chemical class 0.000 description 6
- 239000003054 catalyst Substances 0.000 description 6
- 125000004429 atom Chemical group 0.000 description 5
- 238000000034 method Methods 0.000 description 5
- XEEYBQQBJWHFJM-UHFFFAOYSA-N Iron Chemical compound [Fe] XEEYBQQBJWHFJM-UHFFFAOYSA-N 0.000 description 4
- 230000000996 additive effect Effects 0.000 description 4
- 238000010276 construction Methods 0.000 description 4
- 238000000635 electron micrograph Methods 0.000 description 4
- 229910052731 fluorine Inorganic materials 0.000 description 4
- 229910052759 nickel Inorganic materials 0.000 description 4
- 230000000149 penetrating effect Effects 0.000 description 4
- 238000006243 chemical reaction Methods 0.000 description 3
- 239000011229 interlayer Substances 0.000 description 3
- 238000004519 manufacturing process Methods 0.000 description 3
- 238000005979 thermal decomposition reaction Methods 0.000 description 3
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 description 3
- IJGRMHOSHXDMSA-UHFFFAOYSA-N Atomic nitrogen Chemical compound N#N IJGRMHOSHXDMSA-UHFFFAOYSA-N 0.000 description 2
- YCKRFDGAMUMZLT-UHFFFAOYSA-N Fluorine atom Chemical compound [F] YCKRFDGAMUMZLT-UHFFFAOYSA-N 0.000 description 2
- VEXZGXHMUGYJMC-UHFFFAOYSA-N Hydrochloric acid Chemical compound Cl VEXZGXHMUGYJMC-UHFFFAOYSA-N 0.000 description 2
- NBIIXXVUZAFLBC-UHFFFAOYSA-N Phosphoric acid Chemical compound OP(O)(O)=O NBIIXXVUZAFLBC-UHFFFAOYSA-N 0.000 description 2
- QAOWNCQODCNURD-UHFFFAOYSA-N Sulfuric acid Chemical compound OS(O)(=O)=O QAOWNCQODCNURD-UHFFFAOYSA-N 0.000 description 2
- QVGXLLKOCUKJST-UHFFFAOYSA-N atomic oxygen Chemical compound [O] QVGXLLKOCUKJST-UHFFFAOYSA-N 0.000 description 2
- 230000015572 biosynthetic process Effects 0.000 description 2
- 238000002485 combustion reaction Methods 0.000 description 2
- 239000003822 epoxy resin Substances 0.000 description 2
- 239000011737 fluorine Substances 0.000 description 2
- 125000001153 fluoro group Chemical group F* 0.000 description 2
- 125000000524 functional group Chemical group 0.000 description 2
- 239000004519 grease Substances 0.000 description 2
- 229930195733 hydrocarbon Natural products 0.000 description 2
- 150000002430 hydrocarbons Chemical class 0.000 description 2
- 229910052742 iron Inorganic materials 0.000 description 2
- 239000011159 matrix material Substances 0.000 description 2
- 239000001301 oxygen Substances 0.000 description 2
- 229910052760 oxygen Inorganic materials 0.000 description 2
- 239000002245 particle Substances 0.000 description 2
- 229920000647 polyepoxide Polymers 0.000 description 2
- 239000002994 raw material Substances 0.000 description 2
- 230000035484 reaction time Effects 0.000 description 2
- 229920005989 resin Polymers 0.000 description 2
- 239000011347 resin Substances 0.000 description 2
- UFHFLCQGNIYNRP-UHFFFAOYSA-N Hydrogen Chemical compound [H][H] UFHFLCQGNIYNRP-UHFFFAOYSA-N 0.000 description 1
- HBBGRARXTFLTSG-UHFFFAOYSA-N Lithium ion Chemical compound [Li+] HBBGRARXTFLTSG-UHFFFAOYSA-N 0.000 description 1
- 238000002441 X-ray diffraction Methods 0.000 description 1
- HCHKCACWOHOZIP-UHFFFAOYSA-N Zinc Chemical compound [Zn] HCHKCACWOHOZIP-UHFFFAOYSA-N 0.000 description 1
- 229910000147 aluminium phosphate Inorganic materials 0.000 description 1
- 238000004364 calculation method Methods 0.000 description 1
- 238000003763 carbonization Methods 0.000 description 1
- 125000002915 carbonyl group Chemical group [*:2]C([*:1])=O 0.000 description 1
- 125000003178 carboxy group Chemical group [H]OC(*)=O 0.000 description 1
- 239000003795 chemical substances by application Substances 0.000 description 1
- 239000011248 coating agent Substances 0.000 description 1
- 238000000576 coating method Methods 0.000 description 1
- 239000003086 colorant Substances 0.000 description 1
- 239000002131 composite material Substances 0.000 description 1
- 238000002050 diffraction method Methods 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- KTWOOEGAPBSYNW-UHFFFAOYSA-N ferrocene Chemical compound [Fe+2].C=1C=C[CH-]C=1.C=1C=C[CH-]C=1 KTWOOEGAPBSYNW-UHFFFAOYSA-N 0.000 description 1
- 238000003682 fluorination reaction Methods 0.000 description 1
- 239000000446 fuel Substances 0.000 description 1
- 238000002309 gasification Methods 0.000 description 1
- 229910021389 graphene Inorganic materials 0.000 description 1
- 238000000227 grinding Methods 0.000 description 1
- 239000001257 hydrogen Substances 0.000 description 1
- 229910052739 hydrogen Inorganic materials 0.000 description 1
- 125000000686 lactone group Chemical group 0.000 description 1
- 229910001416 lithium ion Inorganic materials 0.000 description 1
- 229910052757 nitrogen Inorganic materials 0.000 description 1
- 230000003647 oxidation Effects 0.000 description 1
- 238000007254 oxidation reaction Methods 0.000 description 1
- 230000002093 peripheral effect Effects 0.000 description 1
- 230000001737 promoting effect Effects 0.000 description 1
- 239000002296 pyrolytic carbon Substances 0.000 description 1
- 230000002940 repellent Effects 0.000 description 1
- 239000005871 repellent Substances 0.000 description 1
- 229940096017 silver fluoride Drugs 0.000 description 1
- REYHXKZHIMGNSE-UHFFFAOYSA-M silver monofluoride Chemical compound [F-].[Ag+] REYHXKZHIMGNSE-UHFFFAOYSA-M 0.000 description 1
- 238000003756 stirring Methods 0.000 description 1
- 230000010148 water-pollination Effects 0.000 description 1
- 229910052725 zinc Inorganic materials 0.000 description 1
- 239000011701 zinc Substances 0.000 description 1
Images
Classifications
-
- D—TEXTILES; PAPER
- D01—NATURAL OR MAN-MADE THREADS OR FIBRES; SPINNING
- D01F—CHEMICAL FEATURES IN THE MANUFACTURE OF ARTIFICIAL FILAMENTS, THREADS, FIBRES, BRISTLES OR RIBBONS; APPARATUS SPECIALLY ADAPTED FOR THE MANUFACTURE OF CARBON FILAMENTS
- D01F11/00—Chemical after-treatment of artificial filaments or the like during manufacture
- D01F11/10—Chemical after-treatment of artificial filaments or the like during manufacture of carbon
- D01F11/12—Chemical after-treatment of artificial filaments or the like during manufacture of carbon with inorganic substances ; Intercalation
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B82—NANOTECHNOLOGY
- B82Y—SPECIFIC USES OR APPLICATIONS OF NANOSTRUCTURES; MEASUREMENT OR ANALYSIS OF NANOSTRUCTURES; MANUFACTURE OR TREATMENT OF NANOSTRUCTURES
- B82Y30/00—Nanotechnology for materials or surface science, e.g. nanocomposites
-
- D—TEXTILES; PAPER
- D01—NATURAL OR MAN-MADE THREADS OR FIBRES; SPINNING
- D01F—CHEMICAL FEATURES IN THE MANUFACTURE OF ARTIFICIAL FILAMENTS, THREADS, FIBRES, BRISTLES OR RIBBONS; APPARATUS SPECIALLY ADAPTED FOR THE MANUFACTURE OF CARBON FILAMENTS
- D01F9/00—Artificial filaments or the like of other substances; Manufacture thereof; Apparatus specially adapted for the manufacture of carbon filaments
- D01F9/08—Artificial filaments or the like of other substances; Manufacture thereof; Apparatus specially adapted for the manufacture of carbon filaments of inorganic material
- D01F9/12—Carbon filaments; Apparatus specially adapted for the manufacture thereof
- D01F9/127—Carbon filaments; Apparatus specially adapted for the manufacture thereof by thermal decomposition of hydrocarbon gases or vapours or other carbon-containing compounds in the form of gas or vapour, e.g. carbon monoxide, alcohols
Abstract
A fluorinated carbon fiber has a hollow core structure in which a number of hexagonal carbon layers in the shape of a cup having no bottom are stacked. Edges of the hexagonal carbon layers are exposed on the inner and outer surfaces of the fluorinated carbon fiber. In the fluorinated carbon fiber, the exposed edges of the hexagonal carbon layers are fluorinated and have a structure shown by CxFy.
Description
The application comprises the content in Japanese patent application 2001-81742 that proposes March 21 calendar year 2001 and the Japanese patent application 2001-260418 that proposes August 29 calendar year 2001.
Technical field
The present invention relates to fluorinated carbon fibre, use the active material for battery and the solid lubricant of this fluorinated carbon fibre.
Background technology
Carbon fibre with the vapor phase growth manufactured is known.
This carbon fibre is, makes such as the thermal decomposition and the carbon that obtains serves as the staple fibre that nuclear generates with catalyst particles such as ultramicronized iron or tweezers under the temperature of 700 ℃～1000 ℃ of degree of hydrocarbons such as benzene or methane.
As carbon fibre, there is hexagonal carbon layer to be concentric shape growth, there are hexagonal carbon layer and axis to grow perpendicularly, and by changing Vapor Growth Conditions such as catalyst, temperature range, flow, can also produce and have hexagonal carbon layer fish-bone (herring-bone) structure stacked obliquely at a certain angle with respect to fiber axis.
But, because the limitation of vapor growth method itself, on surface, can form sufficient crystallising not, be the thin accumulation horizon that the excess carbon of amorphous shape is piled into the carbon fibre of vapor phase growth manufactured.Because the existence of this accumulation horizon, in general, as this carbon fibre, its activity degree is lower.
In addition, the purposes with the carbon fibre of vapor phase growth manufactured that is the fish-bone structure does not almost obtain exploitation.
Summary of the invention
Thereby the present invention is the invention that the surface active of this carbon fibre that is the fish-bone structure can be fluoridized it, its objective is, fluorinated carbon fibre is provided, use the active material for battery and the solid lubricant of this fluorinated carbon fibre.
For addressing the above problem, a related fluorinated carbon fibre of form of the present invention has the coaxial layer stack structure (coaxial stacking morphlogyof truncated conical tubular graphene layers or truncatedgraphene cone ' s morphology) of frustoconical tubular carbon element stratum reticulare, and each contains hexagonal carbon layer (hexagonal carbon layer) said frustoconical tubular carbon element stratum reticulare.
In other words, this fluorinated carbon fibre has, by a plurality of cup-shaped hexagonal carbon layer in no end structures stacked, cup-shaped stacked (cup stacked) or lamp umbrella stacked (lampshadestacked) that are.The coaxial layer stack structure of this frustoconical tubular carbon element stratum reticulare can form the hollow core (a hollow core with no brige) of not having joint.According to such structure, each frustoconical tubular carbon element stratum reticulare is such structure, that is, have major diameter ring end and minor diameter ring end at axial two ends, expose the edge of hexagonal carbon layer from the minor diameter ring end of the major diameter ring end of outer surface side and inner surface side.In other words, the edge of hexagonal carbon layer that is the inclination of fish-bone structure is stratiform and exposes.
In addition, the carbon fibre of common fish-bone structure is a plurality of being the stacked structure of the cup-shaped hexagonal carbon layer in the end to be arranged, and a fluorinated carbon fibre that form is related of the present invention does not have joint in the scope of tens of nm～tens of μ m length, be hollow form.
Here, if the coaxial layer stack structure of this frustoconical tubular carbon element stratum reticulare is with vapor phase growth, then its outer surface or inner surface will be covered by the accumulating film of the thermally decomposed carbon of surplus (pyrolyticcarbon) very on a large scale.This moment, from least a portion of the major diameter ring end of outer surface side, perhaps the edge of hexagonal carbon layer was exposed at least a portion place of the minor diameter ring end of inner surface side too.
And as a fluorinated carbon fibre that form is related of the present invention, the edge of the said hexagonal carbon layer that it exposed is fluoridized, and has with C
XF
YThe structure of expressing.
As a form of the present invention, also can be for the accumulating film that in carbon fibre vapor phase growth process, is formed at its outer surface or inner surface by processing afterwards with its part or all removal.This be because, this accumulating film is that sufficient crystallising, that be not amorphous shape excess carbon is piled up and formed, the surface of this accumulation horizon does not have active cause.
As a fluorinated carbon fibre that form is related of the present invention, can pass through each major diameter ring end stacked outer surface that forms carbon fibre in the axial direction.At this moment, as long as from more than 2% of its outer surface, preferably the edge of hexagonal carbon layer is exposed in the zone more than 7%.
Similarly, by making the stacked in the axial direction inner surface that forms fluorinated carbon fibre of each minor diameter ring end, the edge of said hexagonal carbon layer can expose from its inner surface.
Like this, just, can fluoridize the edge of the hexagonal carbon layer that exposes from the surfaces externally and internally of carbon fibre as mentioned above.
This fluorinated carbon fibre is applicable to purposes such as the cell active materials, solid lubricant of lithium ion battery etc.
Description of drawings
Fig. 1 is the duplicating figure with the penetrating type electron micrograph of the carbon fibre of the fish-bone structure of vapor phase growth manufactured.
Fig. 2 is the duplicating figure of the enlarged photograph of Fig. 1.
Fig. 3 is the schematic diagram of Fig. 2.
Fig. 4 is under about 530 ℃ of temperature, the duplicating figure of the penetrating type electron micrograph of the carbon fibre of the fish-bone structure of heat treatment after 1 hour in atmosphere.
Fig. 5 is the duplicating figure of the enlarged photograph of Fig. 4.
Fig. 6 is the duplicating figure of the photo after Fig. 5 is further amplified.
Fig. 7 is the schematic diagram of Fig. 6.
Fig. 8 illustrates the carbon fibre of fish-bone structure (sample NO.24PS), in atmosphere, respectively with Raman's frequency spectrum of the carbon fibre of 500 ℃, 520 ℃, 530 ℃, 540 ℃ heat treatments after 1 hour.
Fig. 9 illustrates Raman's frequency spectrum of the carbon fibre of the sample NO.19PS, the sample NO.24PS that expose the edge of hexagonal carbon layer through above-mentioned heat treatment.
Figure 10 illustrates the Raman's frequency spectrum that the above-mentioned carbon fibre that exposes sample NO.19PS, the sample NO.24PS at the edge of hexagonal carbon layer is carried out the carbon fibre after 3000 ℃ the heat treatment.
Figure 11 is the computer graphics of the coaxial layer stack structure of frustoconical tubular carbon element stratum reticulare being showed, the accurate quantum theory calculating of foundation (rigorousquantum theoretical calculation) is drawn.
The accurate quantum theory of the foundation of the hexagonal carbon layer of a unit of stepped construction was calculated the computer graphics of drawing when Figure 12 was a frustoconical tubular carbon element stratum reticulare shown in Figure 11.
Figure 13 is the schematic diagram that the major diameter ring end of the outer surface of stepped construction when being used for to formation frustoconical tubular carbon element stratum reticulare and the minor diameter ring end that forms its inner surface describe.
Figure 14 is used for schematic diagram that the accumulating film at the thermally decomposed carbon that forms of the outer peripheral face of carbon fibre is described on a large scale.
The specific embodiment
Below, best form of implementation of the present invention is elaborated in conjunction with the accompanying drawings.
Carbon fibre with the vapor phase growth manufactured is, makes such as the thermal decomposition and the carbon that obtains serves as the staple fibre that nuclear generates with catalyst particles such as ultramicronized iron or nickel under the temperature of 700 ℃～1000 ℃ of degree of hydrocarbons such as benzene or methane.
As carbon fibre, there is hexagonal carbon layer to be concentric shape growth, there are hexagonal carbon layer and axis to grow perpendicularly, and by changing Vapor Growth Conditions such as catalyst, temperature range, flow, can also produce and have hexagonal carbon layer fish-bone (herring-bone) structure stacked obliquely at a certain angle with respect to fiber axis.
The carbon fibre of common fish-bone structure is a plurality of being the stacked structure of the cup-shaped hexagonal carbon layer in the end to be arranged, and be a plurality of stacked structures of the cup-shaped hexagonal carbon layer in the no end (below, this carbon fibre of no end is called the carbon fibre of fish-bone structure) that are with the carbon fibre of the vapor growth method manufacturing that an embodiment of the present invention was adopted.
That is, this carbon fibre have as among Figure 11 with the coaxial layer stack structure 1 of the frustoconical tubular carbon element stratum reticulare shown in the computer graphics.Each frustoconical tubular carbon element stratum reticulare is formed by hexagonal carbon layer 10 as shown in figure 12.Here, it is closely stacked on axial A that each hexagonal carbon layer 10 shown in Figure 11 is actually, and in Figure 11, show stack density more sparse for ease of describing.
Figure 13 is the schematic diagram of Figure 11, and each hexagonal carbon layer 10 has major diameter ring end 20 and minor diameter ring end 22 at axial two ends.Each major diameter ring end 20 is stacked and form the outer surface 30 of carbon fibre 1 on axial A, and each minor diameter ring end 22 is stacked and form the inner surface 32 of carbon fibre 1 on axial A.Seemingly like this, carbon fibre 1 is the shape with hollow core centre bore 14, the nothing joint.
Below, an example of the manufacture method of carbon fibre 1 shown in Figure 11 is described.
What reactor used is known longitudinal type reactor.
Raw material uses benzene, to produce the partial pressure of about 20 ℃ vapour pressure, sends in the combustion chamber with flow 0.3l/h to reactor by hydrogen stream.Catalyst uses ferrocene, makes its gasification under 185 ℃, with about 3 * 10
-7The concentration of mol/s is sent in the combustion chamber.Reaction temperature is about 1100 ℃, and the reaction time is about 20 fens, obtains the carbon fibre that average diameter is about the fish-bone structure of 100nm.Regulate (according to reactor size change) by flow, reaction temperature, can obtain not having the carbon fibre of the hollow of joint (bridge) by the cup-shaped hexagonal carbon layer in a plurality of no ends scopes stacked, tens of nm～tens of μ m to raw material.
Fig. 1 is that Fig. 2 is the duplicating figure of its enlarged photograph with the duplicating figure of the penetrating type electron micrograph of the carbon fibre of the fish-bone structure of above-mentioned vapor growth method manufacturing, and Fig. 3 is its schematic diagram.
By each figure as can be known, be formed with hexagonal carbon layer 10 excess carbon that cover, that be the amorphous shape that to tilt and pile up the accumulation horizon 12 that forms.The thickness of accumulation horizon 12 is in number nm degree.The 14th, centre bore.
Figure 14 illustrates to the outer surface 30 of carbon fibre 1 is formed with accumulation horizon 14 in a big way situation.As shown in figure 14, at the part place that the outer surface of carbon fibre 1 is not covered by accumulation horizon 12, the edge of hexagonal carbon layer 10 directly exposes from the major diameter ring end 20 that exposes, the activity degree height of this part.The zone that is not covered by accumulation horizon 12 is also arranged on the inner surface of carbon fibre 1, and in this zone, the edge of hexagonal carbon layer 10 directly exposes from the minor diameter ring end 22 that is exposed.
By being formed with the carbon fibre of such accumulation horizon 12, more than 400 ℃, be preferably more than 500 ℃, more preferably more than 520 ℃ under the temperature below 530 ℃, in atmosphere, heat for 1～a few hours, make accumulation horizon 12 oxidations and thermal decomposition takes place, thereby accumulation horizon 12 is removed and then exposed the edge (six membered ring end) of hexagonal carbon layer.
Perhaps, clean carbon fibre with supercritical water and also accumulation horizon 12 can be removed, the edge of hexagonal carbon layer is exposed.
Perhaps, above-mentioned carbon fibre be impregnated in hydrochloric acid or the sulfuric acid, be heated to when stirring about 80 ℃ and also accumulation horizon 12 can be removed with agitator.
Fig. 4 is as mentioned above at the duplicating figure of the penetrating type electron micrograph of the carbon fibre of the fish-bone structure of heat treatment under about 530 ℃ temperature, in atmosphere after 1 hour, Fig. 5 is the duplicating figure of its enlarged photograph, Fig. 6 is that Fig. 7 is its schematic diagram with the duplicating figure of the further photo that amplifies of Fig. 5.
By Fig. 5～Fig. 7 as can be known,, a part of accumulation horizon 12 can be removed, further improve the degree of exposing at the edge (carbon element six membered ring end) of hexagonal carbon layer 10 by carrying out aforesaid heat treatment etc.And residual accumulation horizon 12 can be thought also and to decompose basically, just attached to top.If heat treatment carries out a few hours, perhaps clean with supercritical water again, accumulation horizon 12 also can 100% be removed.
In addition, as shown in Figure 4, carbon fibre 1 is that the cup-shaped hexagonal carbon layer 10 in a plurality of no ends is laminated, and is hollow form at least in tens of nm～tens of mu m ranges.
Hexagonal carbon layer is about 25 degree～35 degree with respect to the inclination angle of center line.
In addition, by Fig. 6 and Fig. 7 as can be known, the outer surface that the edge of hexagonal carbon layer 10 exposes and the position of inner surface, its edge does not align, and presents nm (nanometer) and be small concavo-convex 16 of atom size level.As shown in Figure 2, before accumulation horizon 12 is removed and not obvious, and after by above-mentioned heat treatment accumulation horizon 12 being removed, present concavo-convex 16.
The edge of the hexagonal carbon layer 10 that exposes easily combines with other atom, has high activity degree.Can think, this is because the heat treatment through carrying out in atmosphere, when accumulation horizon 12 is removed, on the edge of the hexagonal carbon layer 10 that exposes, oxygen-containing functional groups such as phenol hydroxyl, carboxyl, quinoid carbonyl, lactone group increase, the hydrophily of these oxygen-containing functional groups, with the high cause of compatibility of other material.
In addition since make hollow structure and have concavo-convex 16, so fixed effect is big.
Fig. 8 illustrates the carbon fibre of fish-bone structure (sample NO.24PS), in atmosphere, respectively with Raman's frequency spectrum of the carbon fibre of 500 ℃, 520 ℃, 530 ℃, 540 ℃ heat treatments after 1 hour.
By above-mentioned heat treatment accumulation horizon 12 is removed this point shown in Fig. 5～Fig. 7, and by Raman's frequency spectrum of Fig. 8 as can be known, owing to there is D peak value (1360cm
-1) and G peak value (1580cm
-1), demonstrating it is carbon fibre, and is the carbon fibre of non-carbonization structure.
That is, can think that the carbon fibre of above-mentioned fish-bone structure has the carbon element wire side Turbostratic (Turbostratic Structure) of (grinding) that staggers.
In this Turbostratic carbon fibre, though have the parallel stepped construction of each carbon element hexagon wire side, the stepped construction that each hexagon wire side staggers on in-plane or rotates does not have the regularity on the crystallography.
The characteristics of this Turbostratic are that other atom etc. is difficult to enter interlayer.This also can be described as an advantage.That is, because material is difficult to enter interlayer, so as previously mentioned, atom etc. year are held on the edge of the hexagonal carbon layer that exposes as previously mentioned, activity degree is high easily, therefore, and can be as holding body performance function in high efficiency year.
Fig. 9 illustrates the Raman's frequency spectrum that makes the carbon fibre of sample NO.19PS, sample NO.24PS that the edge of hexagonal carbon layer exposes through above-mentioned heat treatment.
And Figure 10 illustrates the Raman's frequency spectrum that the above-mentioned carbon fibre that exposes sample NO.19PS, the sample NO.24PS at the edge of hexagonal carbon layer is carried out the carbon fibre after 3000 ℃ the heat treatment (common graphitization processing).
By as can be known shown in Figure 10, even the carbon fibre that the edge of hexagonal carbon layer is exposed carries out graphitization processing, the D peak value can not disappear yet.This explanation is even carry out also graphitization not of graphitization processing.
Though not shown, even from X-ray diffraction, also meeting does not produce 112 diffracted ray, can distinguish also that thus above-mentioned carbon fibre is not by graphitization.
Can think, even why carry out also graphitization not of graphitization processing carbon fibre, be owing to be easy to the cause that graphited accumulation horizon 12 is removed.In addition, learn clearly also that the position of remaining fish-bone structure can graphitization.
As mentioned above, even carbon fibre can graphitization yet under the high temperature atmosphere, this means that carbon fibre has heat endurance.
The edge of the hexagonal carbon layer that is exposed 10 with carbon fibre of above-mentioned characteristic combines with other atom as previously mentioned easily, has high activity degree.
Below, the fluoridizing of carbon fibre that exposes with regard to the edge of said hexagonal carbon layer describes.
The condition of fluoridizing employing is as follows.
That is, said carbon fibre is filled in the nickel system boat, and puts into the nickel pipe (internal diameter is 50mm) of fluoridizing usefulness.With the reaction temperature of fluorine be 340 ℃, the fluorine partial pressure is 460mmHg, nitrogen partial pressure power is 310mmHg.Reaction time is 72 hours.
In addition, for promoting to fluoridize, also can use catalyst such as silver fluoride.
The formation thing all is pure white thread and obtains, and by this color as can be known, has with C
XF
YThe fluorinated carbon fibre of the structure of expressing forms well.
Obviously, fluorination conditions is not limited to the above.
Be known about hexagonal carbon layer with fluoridizing of the carbon fibre of the concentric shape of fiber axis growth.
But this carbon fibre is after fluoridizing, under the effect of the fluorine atom that enters interlayer, hexagonal carbon layer is pulled to that side that fluorine atom enters, its result, and hexagonal carbon layer becomes uneven and damaged because of section, carbon fibre becomes powdery through fluoridizing, and loses fibrous form.Therefore, can't reach need be by the fibrous effect that reaches.
In this regard, can think the above-mentioned carbon fibre that is the fish-bone structure to be hexagonal carbon layer tilt and be with respect to fiber axis can graphited Turbostratic be not reason, even but after fluoridizing, still be fibrous.
As mentioned above, it is fibrous that the fluorinated carbon fibre of this form of implementation keeps, therefore, have good electric conductivity and excellent mechanical strength, can use as the positive electrode of disposable lithium-battery or the additive of positive electrode well, can access than using existing covalent bond type fluorocarbons that the battery of bigger output is arranged, can be used as excellent active material for battery and be used.
In addition, the fluorinated carbon fibre of this form of implementation has been owing to kept fibrous, so can keep the slip between the AB face, in the occasion of using with the matrix material proportioning of resin, grease etc. such as epoxy resin, has the lubricity of excellence.
In addition, the related fluorinated carbon fibre of this form of implementation can be used in the multiple uses such as colorant additive that water and oil repellent agent, non-cementability additives, electric conductivity additives, various composite, developing electrostatic image use and carrier coating additive, fixing roller, phosphoric acid type fuel cell, air/zinc battery, nickel/H accumulator.
Fluorinated carbon fibre involved in the present invention is owing to having kept fibrous, so have good electric conductivity and excellent mechanical strength.
Therefore, can be well use, can access the battery that bigger output is arranged when using existing covalent bond type fluorocarbons, can be used as excellent active material for battery and be used as the positive electrode of disposable lithium-battery or the additive of positive electrode.
And the related fluorinated carbon fibre of this form of implementation has been owing to kept fibrous, so can keep the slip between the AB face, in the occasion of using with the matrix material proportioning of resin, grease etc. such as epoxy resin, has the lubricity of excellence.
Claims (8)
1. fluorinated carbon fibre, it is characterized in that, coaxial layer stack structure with frustoconical tubular carbon element stratum reticulare, each contains hexagonal carbon layer said frustoconical tubular carbon element stratum reticulare, and, have major diameter ring end and minor diameter ring end at axial two ends, at least a portion from said major diameter ring end, the edge that exposes said hexagonal carbon layer, the edge of the said hexagonal carbon layer that exposes is fluoridized, and has with C
XF
YThe structure of expressing.
2. as the said fluorinated carbon fibre of claim 1, it is characterized in that, also expose the edge of said hexagonal carbon layer at least a portion of said minor diameter ring end.
3. as the said fluorinated carbon fibre of claim 2, it is characterized in that, the coaxial layer stack structure of said frustoconical tubular carbon element stratum reticulare forms with vapor phase growth, at least a portion of said major diameter ring end and said minor diameter ring end, formed accumulating film is removed and exposes when vapor phase growth, the other parts of said major diameter ring end and said minor diameter ring end are covered by said accumulation horizon.
4. as the said fluorinated carbon fibre of claim 1, it is characterized in that the coaxial layer stack structure of said frustoconical tubular carbon element stratum reticulare is the hollow core of not having joint and forms.
5. as the said fluorinated carbon fibre of claim 1, it is characterized in that, each said major diameter ring end by said frustoconical tubular carbon element stratum reticulare said axially on the stacked outer surface that forms said fluorinated carbon fibre, from the edge that exposes said hexagonal carbon layer more than 2% of said outer surface.
6. as the said fluorinated carbon fibre of claim 1, it is characterized in that, each said minor diameter ring end by said frustoconical tubular carbon element stratum reticulare said axially on the stacked inner surface that forms said fluorinated carbon fibre, expose the edge of said hexagonal carbon layer from said inner surface.
7. an active material for battery is characterized in that, contains the said fluorinated carbon fibre of claim of one of claim 1 to 6 at least a portion.
8. a solid lubricant is characterized in that, contains the said fluorinated carbon fibre of claim of one of claim 1 to 6 in the part.
Applications Claiming Priority (4)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP81742/01 | 2001-03-21 | ||
| JP2001081742 | 2001-03-21 | ||
| JP260418/01 | 2001-08-29 | ||
| JP2001260418A JP4014832B2 (en) | 2001-03-21 | 2001-08-29 | Fluorinated carbon fiber, battery active material and solid lubricant using the same |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN1388276A CN1388276A (en) | 2003-01-01 |
| CN1228484C true CN1228484C (en) | 2005-11-23 |
Family
ID=26611743
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CNB021074992A Expired - Fee Related CN1228484C (en) | 2001-03-21 | 2002-03-21 | Carbon fluoride fibre, active matter and solid lubricating material for battery using the same |
Country Status (5)
| Country | Link |
|---|---|
| US (1) | US6841610B2 (en) |
| EP (1) | EP1243680B1 (en) |
| JP (1) | JP4014832B2 (en) |
| CN (1) | CN1228484C (en) |
| DE (1) | DE60208101T2 (en) |
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|---|---|---|---|---|
| TW200508431A (en) * | 2003-08-26 | 2005-03-01 | Showa Denko Kk | Crimped carbon fiber and production method thereof |
| US7537682B2 (en) | 2004-03-17 | 2009-05-26 | California Institute Of Technology | Methods for purifying carbon materials |
| JP4747505B2 (en) * | 2004-03-29 | 2011-08-17 | パナソニック株式会社 | Non-aqueous electrolyte battery |
| JP4745634B2 (en) * | 2004-09-14 | 2011-08-10 | 協同油脂株式会社 | Lubricant composition |
| US7505225B2 (en) * | 2005-06-16 | 2009-03-17 | Seagate Technology Llc | Activated carbon fiber filter for a data storage system |
| US7794880B2 (en) * | 2005-11-16 | 2010-09-14 | California Institute Of Technology | Fluorination of multi-layered carbon nanomaterials |
| US8232007B2 (en) | 2005-10-05 | 2012-07-31 | California Institute Of Technology | Electrochemistry of carbon subfluorides |
| US7563542B2 (en) * | 2005-10-05 | 2009-07-21 | California Institute Of Technology | Subfluorinated graphite fluorides as electrode materials |
| US8377586B2 (en) | 2005-10-05 | 2013-02-19 | California Institute Of Technology | Fluoride ion electrochemical cell |
| US20100221603A1 (en) * | 2006-03-03 | 2010-09-02 | Rachid Yazami | Lithium ion fluoride battery |
| US20070218364A1 (en) * | 2005-10-05 | 2007-09-20 | Whitacre Jay F | Low temperature electrochemical cell |
| WO2007126436A2 (en) | 2005-11-16 | 2007-11-08 | California Institute Of Technology | Fluorination of multi-layered carbon nanomaterials |
| US8658309B2 (en) * | 2006-08-11 | 2014-02-25 | California Institute Of Technology | Dissociating agents, formulations and methods providing enhanced solubility of fluorides |
| US20090111021A1 (en) * | 2007-03-14 | 2009-04-30 | Rachid Yazami | High discharge rate batteries |
| CN102203984A (en) * | 2008-11-04 | 2011-09-28 | 加州理工学院 | Hybrid electrochemical generator with a soluble anode |
| US9065144B2 (en) * | 2010-08-12 | 2015-06-23 | Cardiac Pacemakers, Inc. | Electrode including a 3D framework formed of fluorinated carbon |
| US9083048B2 (en) | 2010-08-12 | 2015-07-14 | Cardiac Pacemakers, Inc. | Carbon monofluoride impregnated current collector including a 3D framework |
| JP6020896B2 (en) * | 2011-09-15 | 2016-11-02 | 日産自動車株式会社 | Assembled battery |
| KR101693296B1 (en) | 2011-12-23 | 2017-01-06 | 삼성에스디아이 주식회사 | Cathode active material and method of manufacturing the same and lithium secondary battery including the same |
| JP6408463B2 (en) * | 2013-05-09 | 2018-10-17 | 住友化学株式会社 | Positive electrode material and manufacturing method thereof |
| GB2532035B (en) | 2014-11-06 | 2018-01-10 | Schlumberger Holdings | Lithium carbon fluoride primary battery |
| DE102015200836A1 (en) * | 2015-01-20 | 2016-07-21 | Bayerische Motoren Werke Aktiengesellschaft | Method for determining a surface structure change of at least one carbon fiber |
| CN112234191B (en) * | 2020-09-14 | 2021-09-10 | 方大炭素新材料科技股份有限公司 | Electrode active material, preparation method and lithium primary battery |
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| US112303A (en) * | 1871-02-28 | Improvement in clothes-pins | ||
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| US112306A (en) * | 1871-02-28 | Improvement in paper boxes | ||
| US112298A (en) * | 1871-02-28 | Improvement in steam and hydraulic presses | ||
| US112302A (en) * | 1871-02-28 | Improvement in plows | ||
| US112299A (en) * | 1871-02-28 | Improvement in grain-drills | ||
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| JP3930276B2 (en) | 2001-08-29 | 2007-06-13 | 株式会社Ｇｓｉクレオス | Carbon fiber, electrode material for lithium secondary battery and lithium secondary battery by vapor phase growth method |
-
2001
- 2001-08-29 JP JP2001260418A patent/JP4014832B2/en not_active Expired - Lifetime
-
2002
- 2002-03-18 US US10/098,570 patent/US6841610B2/en not_active Expired - Lifetime
- 2002-03-21 CN CNB021074992A patent/CN1228484C/en not_active Expired - Fee Related
- 2002-03-21 DE DE60208101T patent/DE60208101T2/en not_active Expired - Lifetime
- 2002-03-21 EP EP02006418A patent/EP1243680B1/en not_active Expired - Fee Related
Also Published As
| Publication number | Publication date |
|---|---|
| US6841610B2 (en) | 2005-01-11 |
| JP2002348742A (en) | 2002-12-04 |
| US20020137836A1 (en) | 2002-09-26 |
| DE60208101T2 (en) | 2006-06-29 |
| EP1243680A3 (en) | 2003-04-16 |
| EP1243680B1 (en) | 2005-12-21 |
| EP1243680A2 (en) | 2002-09-25 |
| JP4014832B2 (en) | 2007-11-28 |
| CN1388276A (en) | 2003-01-01 |
| DE60208101D1 (en) | 2006-01-26 |
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